View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 04159U 26071.96053745 +.00000000 +00000-0 +12602-3 0 00001
2 04159 69.9610 66.0418 0111923 78.7216 282.6430 13.72895125 03
| Epoch (UTC): | 12 March 2026 23:03:10 |
| Eccentricity: | 0.0111923 |
| inclination: | 69.9610° |
| perigee height: | 907 km |
| apogee height: | 1072 km |
| right ascension of ascending node: | 66.0418° |
| argument of perigee: | 78.7216° |
| revolutions per day: | 13.72895125 |
| mean anomaly at epoch: | 282.6430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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